CN108974362A - To ammunition locking arrangement and aircraft - Google Patents
To ammunition locking arrangement and aircraft Download PDFInfo
- Publication number
- CN108974362A CN108974362A CN201810805918.1A CN201810805918A CN108974362A CN 108974362 A CN108974362 A CN 108974362A CN 201810805918 A CN201810805918 A CN 201810805918A CN 108974362 A CN108974362 A CN 108974362A
- Authority
- CN
- China
- Prior art keywords
- ammunition
- electromagnet
- handling tube
- locking arrangement
- aircraft
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- 238000010521 absorption reaction Methods 0.000 claims abstract description 10
- 239000004744 fabric Substances 0.000 claims description 3
- 230000005484 gravity Effects 0.000 abstract description 11
- 230000000694 effects Effects 0.000 abstract description 6
- 238000005516 engineering process Methods 0.000 abstract description 3
- 238000001179 sorption measurement Methods 0.000 abstract description 3
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 12
- 229910052742 iron Inorganic materials 0.000 description 6
- 230000009286 beneficial effect Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 230000005611 electricity Effects 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 238000000034 method Methods 0.000 description 1
- 239000000725 suspension Substances 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
- B64D1/02—Dropping, ejecting, or releasing articles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
- B64D1/02—Dropping, ejecting, or releasing articles
- B64D1/08—Dropping, ejecting, or releasing articles the articles being load-carrying devices
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Load-Engaging Elements For Cranes (AREA)
Abstract
The present invention relates to one kind to ammunition locking arrangement and aircraft.Aircraft include body and be arranged on body to ammunition locking arrangement, described to ammunition locking arrangement includes handling tube, the handling tube has for accommodating the accommodating chamber to ammunition, the barrel of handling tube is equipped with electromagnet, and the electromagnet, which has, to be arranged to adsorb the fixed absorption end to ammunition towards accommodating chamber.Electromagnetic adsorption technology is used to ammunition locking arrangement, absorption locking is carried out to ammunition in handling tube using electromagnet, it is needing to discharge when ammunition, it only needs to power off electromagnet, it can be detached from handling tube under the effect of gravity or under the action of self gravity and motor power to ammunition, reduce the volume and weight of locking arrangement, while being also avoided to which lifting lug and hanging are arranged on ammunition, it works simple and reliable, convenient for using on board the aircraft.
Description
Technical field
The present invention relates to one kind to ammunition locking arrangement and aircraft.
Background technique
Conventional on-board to ammunition, generally aboard using lifting lug or hanging suspension, in delivery to ammunition
Detent mechanism is provided on delivery hanger, it is ensured that aboard to the reliable carry of ammunition.In the instant of release, detent mechanism exists
Instruction is lower to release locking, is detached under the effect of gravity or under the action of self gravity and motor power to ammunition
Aircraft enters the autonomous flight stage, to complete to throw operation.
Existing detent mechanism generally comprises mechanical mechanism and electromagnetic actuator, and wherein mechanical mechanism can move,
It moves the constraint by mechanism elastic element, to keep treating the basic carry of ammunition, electromagnetic actuator limited block
Carry out the movement of limit mechanical mechanism.In no dispensing order, mechanical mechanism cannot move opening；Electricity is applied to when launching instruction
When in magnetic actuator, electromagnetic actuator movement, limited block no longer hinders the movement of mechanical mechanism, mechanical mechanism to ammunition oneself
Under the action of body gravity and motor power, overcome the active force of elastic element and open, makes to be detached from aircraft to ammunition.
It needs to carry and launch to ammunition, due to the volume of unmanned plane itself on existing aircraft especially unmanned plane
And load limitation, it needs to keep light weight to ammunition and be assembled convenient for boundling, and existing detent mechanism volume is big, weight
Greatly, there is movement mechanism and locking strength is bigger than normal, while needing to which lifting lug and hanging are arranged on ammunition, work is complicated, no
Convenient for being used on board the aircraft to ammunition.
Summary of the invention
The purpose of the present invention is to provide one kind to ammunition locking arrangement, with solve existing detent mechanism volume it is big,
Weight is big, and work is complicated, is not easy to the problem of using on board the aircraft to ammunition；The present invention also provides a kind of using should be to
The aircraft of ammunition locking arrangement.
In order to solve the above-mentioned technical problem, the technical solution of the invention to ammunition locking arrangement are as follows:
To ammunition locking arrangement, including handling tube, the handling tube has for accommodating the accommodating chamber to ammunition, handling tube
Barrel be equipped with electromagnet, the electromagnet, which has, to be arranged to adsorb the fixed absorption end to ammunition towards accommodating chamber.
The beneficial effect of the technical solution is: using electromagnetic adsorption technology to ammunition locking arrangement, utilizes electromagnet
Absorption locking is carried out to ammunition in handling tube, is needing to discharge when ammunition, it is only necessary to power off electromagnet, wait throw
Handling tube can be detached under the effect of gravity or under the action of self gravity and motor power by throwing object, be reduced
The volume and weight of locking arrangement, while also avoiding working simple and reliable, just to which lifting lug and hanging are arranged on ammunition
In using on board the aircraft.
The electromagnet is arranged on the outer wall of the handling tube.It is connected to convenient for arrangement conducting wire with electromagnet.
The handling tube has at least two and handling tube boundling arranges that the electromagnet is relative to two neighboring handling tube
The line of centres is in tilted layout.It can be convenient for handling tube boundling cloth to avoid interference is generated between the electromagnet on different handling tubes
It sets.
The technical solution of aircraft of the invention are as follows:
Aircraft, including body and be arranged on body to ammunition locking arrangement, it is described to include to ammunition locking arrangement
Handling tube, the handling tube have for accommodating the accommodating chamber to ammunition, and the barrel of handling tube is equipped with electromagnet, the electricity
Magnet, which has, to be arranged to adsorb the fixed absorption end to ammunition towards accommodating chamber.
The beneficial effect of the technical solution is: using electromagnetic adsorption technology to ammunition locking arrangement, utilizes electromagnet
Absorption locking is carried out to ammunition in handling tube, is needing to discharge when ammunition, it is only necessary to power off electromagnet, wait throw
Handling tube can be detached under the effect of gravity or under the action of self gravity and motor power by throwing object, be reduced
The volume and weight of locking arrangement, while also avoiding working simple and reliable, just to which lifting lug and hanging are arranged on ammunition
In using on board the aircraft.
The electromagnet is arranged on the outer wall of the handling tube.It is connected to convenient for arrangement conducting wire with electromagnet.
The handling tube has at least two and handling tube boundling arranges that the electromagnet is relative to two neighboring handling tube
The line of centres is in tilted layout.It can be convenient for handling tube boundling cloth to avoid interference is generated between the electromagnet on different handling tubes
It sets.
Detailed description of the invention
Fig. 1 is the structural schematic diagram to ammunition locking arrangement of aircraft of the invention；
Fig. 2 is the boundling arrangement schematic diagram to ammunition locking arrangement of aircraft of the invention.
It is respectively marked in figure: 1. electromagnet；2. iron plate；3. handling tube；4. to ammunition.
Specific embodiment
Embodiments of the present invention are described further with reference to the accompanying drawing.
The embodiment 1 of aircraft of the invention, as shown in Figures 1 and 2, the aircraft include body (not shown) and
Be arranged on body to ammunition locking arrangement.
It include being assemblied in carry-on handling tube 3 to ammunition locking arrangement, the inner cavity of handling tube 3, which is formed, to be accommodated wait throw
The accommodating chamber of object 4 is thrown, the outer wall of handling tube 3 is equipped with fairshaped box body, and fairshaped box body can reduce aircraft flight
When the resistance that is subject to, be equipped with electromagnet 1 in box body, there is electromagnet 1 accommodating chamber towards handling tube to be arranged to adsorb fixation
Absorption end to ammunition 4.
It is equipped with the shell to ammunition 4, to ammunition 4 in handling tube 3 and is equipped with groove, is equipped with iron plate 2, iron in groove
Plate 2 with the electromagnet 1 on handling tube 3 for being adapted to will be adsorbed in handling tube 3 to ammunition 4；In other embodiments,
It can be omitted groove, iron plate is set up directly on the shell to ammunition 4；The all or part of of shell to ammunition can also
The ferrimagnet that can be adsorbed by electromagnet is thought, to omit iron plate.
The body of aircraft is equipped with the conducting wire of connection electromagnet 1 and the control system of control 1 power on/off of electromagnet, iron plate
2 can be adsorbed by electromagnet 1 so as to be attracted on the inner wall of handling tube 3 to ammunition, in electromagnet 1 when electromagnet 1 is powered
Wait for that ammunition 4 loses constraint when power-off, it can under the effect of gravity to ammunition 4 or self gravity and engine push away
Aircraft is detached under the action of power.
There are four handling tube 3 is total, handling tube 3 arranges that electromagnet 1 is relative to adjacent in array format boundling on board the aircraft
The line of centres of two handling tubes 3 is in tilted layout, and tilt angle is 45 degree, can be to avoid the electromagnet 1 on different handling tubes 3
Between generate interference, convenient for handling tube boundling arrange；In other embodiments, handling tube can also there are two, six, eight etc.
Other quantity can also only have one；The array center that electromagnet 1 can also be formed towards handling tube, electromagnet 1 can also be with
The line of centres with two adjacent handling tubes is in 30 degree, 60 degree, 90 degree of arrangements.
The aircraft in specific application, when ammunition can for air-drop operation when throwing goods and materials, or activity
The throwing present etc. that scene uses, aircraft can be used for the occasion except goods and materials are thrown.It can be with when carrying out throwing operation
To electromagnet input pulse electric current, automatic charging device is set in handling tube to cooperate with pulse current, at upper one wait throw
Throw after object is thrown and conveyed between the pulse spacing of pulse current from trend handling tube it is next to ammunition, thus real
It is now continuous to throw.
The embodiment 2 of aircraft of the invention, the difference from embodiment 1 is that: electromagnet setting is loading in embodiment 1
On the outer wall of cylinder, in the present embodiment, electromagnet also be can be set on the inner wall of handling tube, also can be set in handling tube
Cylinder bottom；Opening can also be set on handling tube, and the absorption end of electromagnet is protruded into the opening and adsorbed with treating ammunition
It is fixed.
In any embodiment of embodiment to ammunition locking arrangement of the invention, specific structure and above-mentioned aircraft
The specific structure to ammunition locking arrangement it is identical, details are not described herein again.
Claims (6)
1. to ammunition locking arrangement, it is characterised in that: including handling tube, the handling tube has for accommodating to ammunition
Accommodating chamber, the barrel of handling tube are equipped with electromagnet, and the electromagnet, which has, to be arranged to adsorb and fix wait throw towards accommodating chamber
The absorption end of object.
2. according to claim 1 to ammunition locking arrangement, it is characterised in that: the electromagnet is arranged in the loading
On the outer wall of cylinder.
3. according to claim 2 to ammunition locking arrangement, it is characterised in that: the handling tube has at least two and fills
Cylinder boundling arrangement is carried, the electromagnet is in tilted layout relative to the line of centres of two neighboring handling tube.
4. aircraft, including body and be arranged on body to ammunition locking arrangement, it is characterised in that: it is described to ammunition
Locking arrangement includes handling tube, and the handling tube has for accommodating the accommodating chamber to ammunition, and the barrel of handling tube is equipped with
Electromagnet, the electromagnet, which has, to be arranged to adsorb the fixed absorption end to ammunition towards accommodating chamber.
5. aircraft according to claim 4, it is characterised in that: the outer wall of the handling tube is arranged in the electromagnet
On.
6. aircraft according to claim 5, it is characterised in that: the handling tube has at least two and handling tube boundling cloth
It sets, the electromagnet is in tilted layout relative to the line of centres of two neighboring handling tube.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810805918.1A CN108974362A (en) | 2018-07-20 | 2018-07-20 | To ammunition locking arrangement and aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810805918.1A CN108974362A (en) | 2018-07-20 | 2018-07-20 | To ammunition locking arrangement and aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108974362A true CN108974362A (en) | 2018-12-11 |
Family
ID=64550538
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810805918.1A Pending CN108974362A (en) | 2018-07-20 | 2018-07-20 | To ammunition locking arrangement and aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108974362A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113928568A (en) * | 2021-11-19 | 2022-01-14 | 中国直升机设计研究所 | Mechanical self-locking type electromagnetic throwing device for unmanned aerial vehicle |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN202340197U (en) * | 2011-11-25 | 2012-07-18 | 河北工业大学 | Electromagnetic-vibration generation device of permanent magnet |
| CN103569361A (en) * | 2013-11-13 | 2014-02-12 | 中国航空工业集团公司西安飞机设计研究所 | Bomb electromagnetic mounting device |
| JP2015193324A (en) * | 2014-03-31 | 2015-11-05 | セコム株式会社 | Flying robot device |
| CN107226191A (en) * | 2017-06-19 | 2017-10-03 | 浙江科技学院 | A kind of many rotor unmanned aircraft chargings are tethered at line automatic releasing device |
| CN206813327U (en) * | 2017-04-11 | 2017-12-29 | 南京伽辽金智能装备有限公司 | Rotary-type electromagnetic launch device is buried in one kind |
| CN207029554U (en) * | 2017-06-07 | 2018-02-23 | 深圳市海旭飞科技有限公司 | A kind of simple unmanned plane disaster relief delivery device |
| CN107961463A (en) * | 2017-12-29 | 2018-04-27 | 广州鼎飞航空科技有限公司 | A kind of quick carry delivery device of unmanned plane fire extinguisher bomb |
| CN208979100U (en) * | 2018-07-20 | 2019-06-14 | 中国空空导弹研究院 | One kind is to ammunition locking arrangement and aircraft |
-
2018
- 2018-07-20 CN CN201810805918.1A patent/CN108974362A/en active Pending
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN202340197U (en) * | 2011-11-25 | 2012-07-18 | 河北工业大学 | Electromagnetic-vibration generation device of permanent magnet |
| CN103569361A (en) * | 2013-11-13 | 2014-02-12 | 中国航空工业集团公司西安飞机设计研究所 | Bomb electromagnetic mounting device |
| JP2015193324A (en) * | 2014-03-31 | 2015-11-05 | セコム株式会社 | Flying robot device |
| CN206813327U (en) * | 2017-04-11 | 2017-12-29 | 南京伽辽金智能装备有限公司 | Rotary-type electromagnetic launch device is buried in one kind |
| CN207029554U (en) * | 2017-06-07 | 2018-02-23 | 深圳市海旭飞科技有限公司 | A kind of simple unmanned plane disaster relief delivery device |
| CN107226191A (en) * | 2017-06-19 | 2017-10-03 | 浙江科技学院 | A kind of many rotor unmanned aircraft chargings are tethered at line automatic releasing device |
| CN107961463A (en) * | 2017-12-29 | 2018-04-27 | 广州鼎飞航空科技有限公司 | A kind of quick carry delivery device of unmanned plane fire extinguisher bomb |
| CN208979100U (en) * | 2018-07-20 | 2019-06-14 | 中国空空导弹研究院 | One kind is to ammunition locking arrangement and aircraft |
Non-Patent Citations (2)
| Title |
|---|
| 邵帆; 牛绿伟: "导弹模拟系统的仿真与实现" * |
| 高慧杰;张建;周志卫;盛德兵;: "悬挂发射装置弹射力的光学测量方法", no. 02 * |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113928568A (en) * | 2021-11-19 | 2022-01-14 | 中国直升机设计研究所 | Mechanical self-locking type electromagnetic throwing device for unmanned aerial vehicle |
| CN113928568B (en) * | 2021-11-19 | 2023-04-18 | 中国直升机设计研究所 | Mechanical self-locking type electromagnetic throwing device for unmanned aerial vehicle |
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